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Optimization procedure of blade cooling system

Wybrane pełne teksty z tego czasopisma
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper discuses the problem of cooling system optimization within a gas turbine vane. The analysis involves the optimization of the location and size of internal cooling passages (circular and noncircular) within the vane. Shape of a noncircular passage is modelled with Bezier's splines. The analysis is performed by means of the genetic algorithm for the optimization task and FEM for heat transfer predictions within the component. In the present study the vane profile is assumed as aerodynamically optimal.
Rocznik
Strony
63--82
Opis fizyczny
Wz., wykr., tab., rys.,Bibliogr. 14 poz.
Twórcy
autor
autor
  • Silesian University of Technology, Institute of Power Engineering and Turbomachinery, ul. Konarskiego 18, 44-100 Gliwice, Poland
Bibliografia
  • [1] SHOKO ITO ET AL.; Conceptual design and cooling blade development of 1/00°C - class high - temperature gas turbine, ASME Paper GT 2003-38352.
  • [2] BOHN D., KRÜGER U., KUSTERER K.: Conjugate heat transfer: an advanced computational method for the cooling design of modern gas turbine blades and vanes, Heat Transfer in Gas Turbines (Eds. B, Sunden, M. Faghri), WIT Press, Southampton 2001, 58-108.
  • [3] Analytical and Experimental Evaluation of the Heat Transfer Distribution Over the Surfaces of Turbine Vanes, NASA Report, 1983
  • [4] FACCHINI B., MAGI A., SCOTTI DEL GRECO A.: Conjugate heat transfer simulation of radially cooled gas turbine vane, ASME Paper GT 2004-54213.
  • [5] MONTOMOLI F., DELLA GATTA S., ADAMI S., MARTELLI F.: Conjugate Heat Transfer Modeling in Film Cooled Blades, ASME Paper GT 2004-53177.
  • [6] FEDRIZZI, R., ARTS, T.: Investigation of the conjugate convective-conductive thermal behavior of a rib-roughened internal cooling channel, ASME Paper GT2004-53046.
  • [7] KUSTERER K., BOHN D., SUGIMOTO T., TANAKA R.: Conjugate Calculation for a Film-Cooled Blade Under Different Operating Conditions, ASME Paper GT 2004-53719.
  • [8] MARTIN T. J., DULIKRAVICH G. S.: Aero-Thermo-Elastic Concurrent Optimization of Internally Cooled Turbine Blades, in Coupled Field Problems, Series of Advances in Boundary Elements (eds. Kassab A., Aliabadi M.), WIT Press, Boston 2001, 137-184.
  • [9] DENNIS B., EGOROV I., DULIKRAVICH G., YOSHIMURA S.: Optimization of a Large Number Coolant Passages Located Close to the Surface of a Turbine Blade, ASME Paper GT2003-38051.
  • [10] HAASENRITTER A., WEIGAND B.: Optimization of the rib structure inside a 2D cooling channel, ASME Paper GT2004-53187.
  • [11] FAVORETTO C., FUNAZAKI K.: Application of genetic algorithms to design of an internal turbine cooling system, ASME Paper GT2003-38408.
  • [12] GOLDBERG D.: Genetic Algorithms in Search, Optimization, and Machine Learning, Addison-Wesley, Reading 1989.
  • [13] ZECCHI S., ARCANGELI L., FACCHINI B., COUTANDIN D.: Features of cooling systems simulation tool used in industrial preminary design stage, ASME Paper GT2004-53547.
  • [14] BRONSZTEJN I. N., SIEMIENDIAJEW K. A.: Mathematics — Encyclopedic Handbook, PWN, Warszawa 1990 (in Polish).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BGPK-1546-6072
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